View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 57678U 26145.66668980 +.00000000 +00000-0 +94297-3 0 00007
2 57678 53.1602 196.3618 0001719 62.6548 12.7644 15.34403506 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001719 |
| inclination: | 53.1602° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 196.3618° |
| argument of perigee: | 62.6548° |
| revolutions per day: | 15.34403506 |
| mean anomaly at epoch: | 12.7644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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